Apparatus and method for suppressing double images on a combiner head-up display

ABSTRACT

A head-up display system and method are provided that suppress double images from a combiner by eliminating or reducing a reflection of a refracted image from the back surface of the combiner. The combiner contains a tilted axis polarizing structure that attenuates transmittance and subsequent reflection of a refracted polarized projector image but maintains high transmittance for the forward external scene imagery.

TECHNICAL FIELD

The present invention generally relates to head-up displays (HUDs), andmore particularly relates to a HUD that suppresses (reduces oreliminates) double images from a combiner.

BACKGROUND

Head-up displays (HUDs) are becoming increasingly popular in theaerospace industry. Known HUDs typically include at least a projector, acombiner, and an image generator. The projector receives images suppliedfrom the image generator, and the HUD will typically include an opticalcollimator, such as a convex lens or concave mirror, to produce an imagethat is perceived to be at infinity or other far distance.

The combiner reflects the image projected by the projector in such a wayas to see the field of view and the projected infinity image at the sametime. The combiner is typically a very precisely designed and controlledoptical element and may be flat or curved. Some combiners may also havespecial coatings that reflect certain wavelengths of light projectedonto it from the projector while allowing other wavelengths of light topass through.

Traditional prior art HUDs typically rely on sophisticated optics tomeet the performance requirements for avionic use. These performancerequirements include precise angular control and uniformity over an exitpupil or head box that is large enough to encompass both eyes of a pilotor other user. As an example, the size, weight and cost of a bulkyoverhead unit (OHU) may be driven to a large extent by the requiredperformance levels.

Referring to FIG. 1, a known HUD 100, for example, as included in anaircraft, includes a projector 102, and a combiner 104, for example apartially reflective element proximate the windscreen of the aircraft,that directs images 113 and 116 to a receiver 106, for example, aperson's eyes. In the traditional aircraft HUD, the combiner 104 istypically a very precisely designed and controlled separate opticalelement, and includes a front, or inner, surface 108, and a back, orouter, surface 110. The projector 102 projects an image 112 onto thefront surface 108, wherein the desired image 113 is reflected backtoward the receiver 106 and some of the image 112 propagates through thecombiner 104, reflecting off of the back surface 110 as a potentiallyundesired image 116. The images 113 and 116 can present a double imageto the receiver 106 unless measures are taken to either reduce thereflectivity of back surface 110 relative to front surface 108 or toeffectively align the two reflected images. The outside view 118 entersthe combiner 104 at the back surface 110 and propagates through thecombiner 104 to the receiver 106 combined with the reflected HUD images113 and 116. Whereas combiner 104 has been described in this example asan optical element that is separate from and proximate the windscreen orwindshield, certain vehicular HUD configurations, most notablyautomotive HUDs, may utilize the windshield or windscreen as thecombiner rather than using a separate element. These will also involvethe possibility of multiple visible reflected images.

Very often, and particularly with curved combiners, carefully designedand deposited coatings may be applied to the front and back surfaces.There are multiple objectives in selecting these coatings. One typicalgoal is to provide adequate reflectance of the HUD imagery while at thesame time maintaining high “see-through” transmittance of the forwardscene. Partially reflecting coatings would generally be applied on oneof the surfaces, most commonly the front surface. Other objectives mayinclude maximizing luminance of the HUD reflection while minimizingcolor tinting for the forward scene. Yet another objective may be tominimize any undesired visual artifacts associated with reflections fromthe rear surface of the combiner. As an example, the combiner surfacemight have a narrow band reflective multilayer interference coating, andthe rear surface might have an anti-reflection coating of some type.However, when utilizing a vehicle windshield or windscreen as acombiner, the practicality and effectiveness of such a rear coatingcould be affected, for example due to rain or other contaminant buildup.

Accordingly, it is desirable to provide a HUD that suppresses doubleimages from the combiner by eliminating or reducing a reflection of theHUD display from the back surface of the combiner. Furthermore, otherdesirable features and characteristics of the exemplary embodiments willbecome apparent from the subsequent detailed description and theappended claims, taken in conjunction with the accompanying drawings andthe foregoing technical field and background.

BRIEF SUMMARY

A HUD system and method eliminates or reduces reflection of the HUDimage by the back (outer) surface of a combiner.

In an exemplary embodiment, a head-up display system for overlaying aprojected image onto an external scene image, the head-up display systemcomprising a combiner having a first surface and a second surface andincluding a uniaxially absorbing polarizing structure; a polarized imagegeneration system configured to project polarized light onto thecombiner; and the uniaxially absorbing polarizing structure having alocal absorption axis and disposed one of on the combiner to define thefirst surface, or within the combiner between the first surface and theback surface, the local absorption axis being substantially aligned ateach point with the propagation direction of the external scene imagetransmitted through the combiner toward a design eye point for thehead-up display system, the combiner configured to reflect from thefirst surface a first portion of the polarized light from the imagegeneration system toward the design eye point for the head-up displaysystem, and the uniaxially absorbing polarizing structure configured tosubstantially absorb a second portion of the polarized light from theimage generation system.

In another exemplary embodiment, a head-up display system, comprises acombiner comprising a transparent layer having a first surface and asecond surface and configured to allow a first image to passtherethrough in a first direction; and a polarizing layer disposed onone of the first surface or within the transparent layer, the firstsurface defining a tangential plane at each point of the surface, andthe polarizing layer having a uniaxial absorption axis at a non-zeroangle with respect to the tangential plane, thereby configured tosuppress a refracted image created by a polarized image passing throughthe transparent layer and reflecting off the second surface; and apolarized image generation system configured to project the polarizedimage onto the combiner, wherein a reflected image and the first imageare combined in the first direction.

In yet another exemplary embodiment, a method comprises projecting apolarized image from a polarized image generation system onto apolarizing structure disposed in association with a combiner, wherein afirst portion of the polarized image is reflected in a first directionby a first surface of the combiner prior to reaching the polarizingstructure; reducing a second portion of a refracted polarized imagereflected from a second surface of the combiner by attenuating thesecond portion of the polarized image as it passes through thepolarizing structure; and allowing a non-polarized image to pass throughthe combiner and the polarizing layer in the direction of the reflectedfirst portion without being polarized by the polarizing structure.

BRIEF DESCRIPTION OF THE DRAWINGS

The present invention will hereinafter be described in conjunction withthe following drawing figures, wherein like numerals denote likeelements, and

FIG. 1 is a diagram of a known HUD system suitable for use in anaircraft or other vehicle;

FIG. 2 is a first exemplary embodiment of a HUD system that suppressesdouble images;

FIG. 3 is a second exemplary embodiment of a HUD system that suppressesdouble images;

FIG. 4 is a third exemplary embodiment of a HUD system that suppressesdouble images;

FIG. 5 is a fourth exemplary embodiment of a HUD system that suppressesdouble images;

FIG. 6 is an exemplary embodiment of a combiner that suppresses doubleimages;

FIG. 7 is another exemplary embodiment of a combiner system thatsuppresses double images; and

FIG. 8 is a flow diagram of an exemplary method in accordance with theexemplary embodiments.

DETAILED DESCRIPTION

The following detailed description is merely illustrative in nature andis not intended to limit the embodiments of the subject matter or theapplication and uses of such embodiments. Any implementation describedherein as exemplary is not necessarily to be construed as preferred oradvantageous over other implementations. Furthermore, there is nointention to be bound by any expressed or implied theory presented inthe preceding technical field, background, brief summary, or thefollowing detailed description.

In this document, relational terms such as first and second, and thelike may be used solely to distinguish one entity or action from anotherentity or action without necessarily requiring or implying any actualsuch relationship or order between such entities or actions. Numericalordinals such as “first,” “second,” “third,” etc. simply denotedifferent singles of a plurality and do not imply any order or sequenceunless specifically defined by the claim language. The sequence of thetext in any of the claims does not imply that process steps must beperformed in a temporal or logical order according to such sequenceunless it is specifically defined by the language of the claim. Theprocess steps may be interchanged in any order without departing fromthe scope of the invention as long as such an interchange does notcontradict the claim language and is not logically nonsensical.

For the sake of brevity, conventional techniques related to opticalsystems, and other functional aspects of certain systems and subsystems(and the individual operating components thereof) may not be describedin detail herein. It should be noted that many alternative or additionalfunctional relationships or physical connections may be present in anembodiment of the subject matter.

Although embodiments described herein are specific to aircraft HUDsystems, it should be recognized that principles of the inventivesubject matter may be applied to other vehicle display systems such asHUDs in sea going vessels and automobiles, and that some or all of theimages may be transmitted as frequencies other than visible light.

Techniques and technologies may be described herein in terms offunctional and/or block components, and with reference to symbolicrepresentations of operations, processing tasks, and functions that maybe performed by various computing components or devices. Suchoperations, tasks, and functions are sometimes referred to as beingcomputer-executed, computerized, software-implemented, orcomputer-implemented. In practice, one or more processor devices cancarry out the described operations, tasks, and functions by manipulatingelectrical signals representing data bits at memory locations in thesystem memory, as well as other processing of signals. It should beappreciated that the various block components shown in the figures maybe realized by any number of hardware, software, and/or firmwarecomponents configured to perform the specified functions.

During the course of this description, like numbers may be used toidentify like elements according to the different figures thatillustrate the various exemplary embodiments.

Referring to FIG. 2, a functional block diagram of one embodiment of aHUD system 200 is depicted and includes a polarized image generationsystem 201, and a combiner 204 having a polarizing layer 205 positionedadjacent to a front surface 208. While the polarizing layer 205 ispositioned adjacent to the front surface of the combiner 204 in thisexemplary embodiment, the polarizing layer 205 may alternatively beformed or distributed elsewhere within the combiner. The polarized imagegeneration system 201 may include, for example, a projector 202 and apolarizer (polarizing filter) 203 for projecting the polarized image212.

In this exemplary embodiment, the combiner 204 is a windscreen in anaircraft; however, in other exemplary embodiments, the combiner 204 maybe a transparent layer that may be used for other purposes other than todeflect wind. In accordance with the exemplary embodiments, the combiner204 may be implemented using any one of numerous known combiners, orcombiners hereinafter developed, suitable for rendering textual,graphic, and/or iconic information in a format viewable by the operator.For example, further benefits of the described configurations can beconsidered in addition to the benefits described for HUD use.

The projector 202 may be variously configured to implement its functionof projecting information desired by the user, for example, informationrelating to flight parameters or conditions when used in an aviationenvironment. Specifically, the HUD system 200 may be configured toprocess the current flight status data for the host aircraft. In thisregard, the sources of flight status data generate, measure, and/orprovide different types of data related to the operational status of thehost aircraft, the environment in which the host aircraft is operating,flight parameters, and the like. The data provided by the sources offlight status data may include, without limitation: airspeed data;groundspeed data; altitude data; attitude data, including pitch data androll data; yaw data; geographic position data, such as GPS data;time/date information; heading information; weather information; flightpath data; track data; radar altitude data; geometric altitude data;wind speed data; wind direction data; etc.

It will be appreciated that the projector 202 may be variouslyimplemented and may be conformal-capable. The term “conformal-capable”as used herein indicates that the described embodiment(s) can beconfigured to display imagery which is substantially conformal to aforward scene observable through the combiner or other image combinerelement, although the system may also be used in non-conformal modes andapplications as well as configurations with little or no see-through toan outside scene.

The polarizer 203 is positioned over or otherwise combined with theprojector 202 for polarizing the electromagnetic radiation of an image212. Alternately, the polarizer 203 may be omitted if the polarizedimage 212 is inherently polarized by the polarized image generationsystem 201. While the preferred polarizer 203 is a uniaxial absorbingpolarizer element, this is not intended to be limiting and other typesof polarizing elements (e.g., reflective, dielectric, and beam splittingpolarizers, wire-grid polarizers, or combinations of cholestericpolarizers with appropriate quarter-wave retardation films) can be usedfor the polarizer 203.

It should be understood that FIG. 2 is a simplified representation of adisplay system 200 for purposes of explanation and ease of description,and FIG. 2 is not intended to limit the application or scope of thesubject matter in any way. In practice, the display system 200 mayinclude numerous other devices and components, either alone or incombination with additional systems, for providing additional functionsand features, as will be appreciated in the art.

In accordance with the exemplary embodiments, the apparatus and methoddescribed herein leverage the fact that polarization in general is athree-dimensional parameter rather than a two-dimensional parameter.FIG. 2 is an exemplary embodiment wherein light 218 (which may bereferred to as an outside view) from a forward exterior scene, andhaving arbitrary polarization, is transmitted through the combiner 204toward the eye 206, and is combined with the reflected image 213. Animage 212 from the polarized image generation system 201 (collimationoptics are optional) is directed toward the combiner 204 and a firstportion of the image 212 is reflected as the image 213 (combined withthe outside view 218) toward the eye 206. A second portion 214(“refracted ray”) enters the combiner and part 215 of that is reflectedby the back surface 210 of the combiner. This refracted ray 214 whichthen becomes the reflected ray 215 may proceed toward the eye as apotential double image, ray 216; however, the invention described hereineliminates, or substantially reduces, the second portion 214, 215, 216,and therefore the double image as discussed hereinafter. It should benoted that while the various figures show the reflecting surface orcomponent of the combiner 204 as being the front surface 208, therecould optionally be additional layers on the front surface. It is notrequired that the front, or reflecting, surface of the combiner be anexterior surface that interfaces to air, though the embodiments asdisclosed assume that the rays associated with image 212 will reach thatfront, or reflecting, surface prior to reaching polarizing layer 205.

While FIG. 2 traces the path(s) of a single ray from the display, thepresent invention works well with multiple image problems. For anexample having multiple images, see FIG. 2 of U.S. Pat. No. 5,013,134,which shows how two rays emitted from a common point on an(uncollimated) image can end up on separate positions on the viewer'sretina. That patent also teaches a tapered windshield approach (see FIG.6) which allows superimposing the ghost image on top of the primaryimage, at least to some degree over a certain range of angles andpositions. Another well-established special case where double images aresuperimposed and overlay each other is in the case of well-collimatedimagery reflecting from flat and parallel surfaces.

The embodiment of FIG. 2 addresses the multiple image issue by includinga polarizing layer 205 having a tilted axis 209 (represented by theshort parallel lines). For a uniaxial absorbing axis within thiscombiner 204, any light with a propagation direction substantiallyaligned with the tilted axis 209 is not absorbed, since bothpolarization axes of the light are orthogonal to the tilted axis 209.The tilted axis 209 is oriented at a non-zero angle with respect to theplane of the polarizing layer 205 (or, if curved, the local plane ortangent plane associated with the polarizing layer in that particularvicinity or location).

However, the refracted ray 214 from the polarized image generationsystem 201 can have at least a portion of its light polarized along,i.e. the electric field is not orthogonal to, the tilted axis 209 and isthereby attenuated by the tilted axis 209. By suitably adjusting theoutput polarization of the polarized image generation system 201, e.g.favoring P-polarization at the combiner, as well as the polarizingefficiency of the tilted axis 209, the second surface 210 reflection 216can be effectively reduced or eliminated.

In accordance with another exemplary embodiment, the tilted axispolarizer 205 is an element that is applied to the combiner 204 as inFIG. 2. The tilted axis polarizer 205 could be permanently laminated, oralternately could be an applied film, covering the viewing area of thecombiner 204, or optionally a larger area of the combiner 204.

An exemplary embodiment of FIG. 3 comprises the polarizer 205, with itstilted axis 209, immersed within the combiner 204, for example inside ofa multi-layer combiner 204.

In still another exemplary embodiment, the tilted axis 209 could benormal to the local plane of the polarizing layer 205 (see FIG. 4wherein the short parallel lines 209 are perpendicular to the polarizinglayer 205 plane), i.e., a homeotropic axis or z-axis, which is not fullyaligned with the internal propagation angles for the outside view,provided that the outside view attenuation from the design eye point(DEP) remains acceptable. While both the outside view 218 and thereflection 215, if any, of refracted ray 214 would see some slightattenuation by the layer 205, the refracted ray 214 could still undergosubstantial attenuation, depending of course upon the detailedreflection and refraction angles involved.

Additional coatings could be incorporated into/onto the film or combinerto selectively modify which wavelengths or polarizations arepreferentially reflected by the desired reflection surface. Referring toFIG. 5, the combiner 204 includes coatings 205′, and 205″ in addition topolarizing layer 205. This may be desirable, especially if the polarizedimage generation system 201 image 212 is P-polarized for the combiner204 reflection. Alternately, polarization retardation layers 205′, 205″could be used, for example, to reflect incident light havingS-polarization, but then rotating the polarization of refracted rays tobe more effectively absorbed. Similarly, retardation layers could beadded between tilted axis polarizer 205 and the rear surface 210 ofcombiner 204 to rotate the polarization of light passing through thatregion within the HUD system 200.

Referring to the exemplary embodiment of a curved combiner shown in FIG.6, the tilt of the polarizing axis 209 could be varied across the areaof the combiner 204 such that its axis is aligned with the line of sightfor a range of angles from the DEP. A similar variation could also beapplied in the case of a flat combiner as depicted in several earlierfigures.

Besides depicting a single polarizing layer having tilted uniaxialorientation, the diagram of FIG. 6 can also be interpreted to portray anadditional embodiment which utilizes conventional polarizer technology.Rather than interpreting the short lines within the polarizing layer asa tilted absorption axis, those lines could represent conventionalpolarizer sheets or sections immersed within a bulk layer. As oneexample, such a bulk layer could be several millimeters thick.Additional supporting layers, such as glass, are likely present as well,though not shown in FIG. 6 or 7. While such polarizer sections willabsorb a portion of the incident light having polarization which is notorthogonal to the linear axes as shown, they will remain substantiallytransparent to the viewer's eye since each of those ray directions willhave both polarizations substantially normal to the linear axes asshown. This embodiment allows suppression of the multiple reflectionsusing conventional polarizers, but at the same time preserves the hightransmittance, for example, greater than 80% transmittance, typicallyrequired of HUDs in certain applications such as aircraft pilotage. Ofimportance would be to carefully index-match the materials and to avoidair pockets which could lead to distracting visual artifacts. Theviewing geometry should adequately match the design eye point (DEP)line-of-sight arrangement to prevent visual artifacts. Here, the DEP isconsidered to be the nominal location for the pilot's eye 206 whenviewing the outside scene.

Depending upon the thickness and detailed projection geometry, this“stacked” conventional polarizer structure can potentially be fairlysparse, with an appreciable separation between the stacked layers.

This alternate configuration can be interpreted even more broadly byassuming that the absorbing axes of the conventional sheets or sectionsare normal to the page, such that they would preferentially absorbincident rays having S-polarization. In this case, however, it will beeven more important that the layers match the DEP line-of-sight to avoidthe appearance of bright and darker bands in the combiner transmittanceof the outside forward scene.

Still referring to FIG. 6 and in yet another exemplary embodiment, eachof the stacked layers could include crossed polarizers, which wouldsubstantially absorb both polarizations refracting into said layer. Asimpler method for achieving this would be for the immersed and stackedlayers, or even fibers, to be quite thin and deeply tinted or evenopaque black, without the need for polarizer-type functionality. Thiswould be somewhat analogous to the use of extramural absorption (EMA)material in fiber optic faceplates to reduce off-axis propagation,immersed louvers to reduce off-axis throughput, or similarly Sollerslits as used within X-ray collimators, but with notable distinctions interms of the useful embodiment(s) in conjunction with the front surfaceHUD reflection. As with the stacks described above which absorbS-polarization, the alignment tolerances would be necessarily tight ifhigh transmittance and minimal transmittance modulation of the DEPline-of-sight are important.

Referring to FIG. 7, the adjusted tilt angles of, for example FIG. 6,could also be achieved by using sections or sheets 220 of a homeotropicpolarizer. In this case, the individual sheets would be rotatedapproximately ninety degrees relative to the case of conventionalpolarizer sections in FIG. 6 such that the homeotropic absorbing axis ofeach section would align substantially with the nominal line of sight atthat location. In such a case, it would be preferable to stagger oroverlap the sections such that there are no apparent gaps in coveragefor the refracted rays.

The polarizing layer (or related polarizing structure, several of whichhave been disclosed herein) 205 would be effective for use on either adual-purpose windscreen/combiner, or a combiner that is separate fromthe windscreen or windshield. In the case of it being a separateelement, there would typically be another transparent windscreenstructure proximate and to the left of the combiner 204 in the variousFIGS. 2 through 7, though not explicitly shown. Depending upon therelative angles between such a separate windscreen and the combiner, thewindscreen could potentially contribute additional multiple reflectionsof the HUD imagery, but the present invention would attenuate oreliminate those reflections as well since it functions by attenuatingthe rays before they would reach such a separate windscreen, if present.

While FIGS. 1-7 show various flat and curved combiner regions, it shouldbe understood that alternate combiner curvatures can be considered aswell. For example, when reference is made to a “plane” defined by asurface, a corresponding interpretation for a curved surface would be alocal plane or tangent plane for that point being referenced.

In a preferred embodiment, the tilted axis structure is photometricallystable, for example, by the use of highly stable dichroic dye(s), oriodine-based structures (as in most conventional polarizing films).However, various embodiments are possible for fabricating such apolarizer having a tilted absorption axis, including an absorption axiswhose tilt varies.

As an example, various methods for modifying the tilt angle fromhomeotropic are possible, such as the use of fixed or variable appliedfields during the crosslinking (or drying) of an orientable hostmaterial containing suitable dichroic guest dye/absorbing materials.

An alternate method for achieving or modifying tilt could be through theuse of mechanical shear forces as applied to substantially homeotropicpolarizing films. The shear forces could be applied locally or across alarge film area. Yet another is by making the film to conform with aparticular surface.

Another significant benefit of the present invention is that it does notrely upon the characteristics of the reflection by the exterior surface210, since it attenuates the refracted rays 214 before reaching thatexterior surface 210. For example, a mist or rain on the exteriorsurface 210 could lead to diffuse scatter of HUD light 212 (as therefracted rays 214) that reaches it, but this disclosed approach wouldattenuate such light 214 before reaching that exterior surface 210.

The methods described herein may of course be used in conjunction withother methods, known or not yet described, for reducing the undesiredreflections that impact the effectiveness and/or clarity of the viewedimage.

FIG. 8 is a flow chart that illustrates an exemplary embodiment of amethod 800 suitable for use with a display system, for example, a flightdeck display or automobile display. For illustrative purposes, thefollowing description of method 800 may refer to elements mentionedabove in connection with preceding FIGS. It should be appreciated thatmethod 800 may include any number of additional or alternative tasks,the tasks shown in FIG. 8 need not be performed in the illustratedorder, and method 800 may be incorporated into a more comprehensiveprocedure or method having additional functionality not described indetail herein. Moreover, one or more of the tasks shown in FIG. 8 couldbe omitted from an embodiment of the method 800 as long as the intendedoverall functionality remains intact.

In accordance with the exemplary method of FIG. 8, the method 800comprises projecting 802 a polarized image from a polarized imagegeneration system onto a polarizing structure disposed within acombiner, wherein a first portion of the polarized image is reflected ina first direction by the combiner prior to reaching the polarizingstructure; reducing 804 a second portion of a refracted polarized imagereflected from a back surface of the combiner by attenuating the secondportion of the polarized image as it passes through the polarizingstructure; and allowing 806 a non-polarized image to pass through thecombiner and the polarizing layer without being polarized by thepolarizing structure.

Benefits, other advantages, and solutions to problems have beendescribed above with regard to specific embodiments. However, thebenefits, advantages, solutions to problems, and any element(s) that maycause any benefit, advantage, or solution to occur or become morepronounced are not to be construed as a critical, required, or essentialfeature or element of any or all the claims. As used herein, the terms“comprises,” “comprising,” or any other variation thereof, are intendedto cover a non-exclusive inclusion, such that a process, method,article, or apparatus that comprises a list of elements does not includeonly those elements but may include other elements not expressly listedor inherent to such process, method, article, or apparatus.

While at least one exemplary embodiment has been presented in theforegoing detailed description, it should be appreciated that a vastnumber of variations exist. It should also be appreciated that theexemplary embodiment or exemplary embodiments are only examples, and arenot intended to limit the scope, applicability, or configuration of theinvention in any way. Rather, the foregoing detailed description willprovide those skilled in the art with a convenient road map forimplementing an exemplary embodiment of the invention, it beingunderstood that various changes may be made in the function andarrangement of elements described in an exemplary embodiment withoutdeparting from the scope of the invention as set forth in the appendedclaims.

What is claimed is:
 1. A head-up display system for overlaying aprojected image onto an external scene image, the head-up display systemcomprising: a combiner having a first surface and a second surface andincluding a uniaxially absorbing polarizing structure; a polarized imagegeneration system configured to project polarized light onto thecombiner; and the uniaxially absorbing polarizing structure having alocal absorption axis and disposed on the combiner to define the firstsurface, or within the combiner between the first surface and the secondsurface, the local absorption axis being normal to the first surface,the combiner configured to reflect from the first surface a firstportion of the polarized light from the image generation system toward adesign eye point for the head-up display system, and the uniaxiallyabsorbing polarizing structure configured to substantially absorb asecond portion of the polarized light from the image generation system.2. The head-up display system of claim 1 wherein the uniaxial absorptionaxis is parallel to an internal propagation vector through the combinerfor the external scene image directed toward the design eye point. 3.The head-up display system of claim 1 wherein the uniaxially absorbingpolarizing structure has greater than 50%, transmittance at each visiblewavelength for rays propagating from the external scene toward thedesign eye point.
 4. The head-up display system of claim 1 wherein theuniaxially absorbing polarizing structure has greater than 70%transmittance at each visible wavelength for rays propagating from theexternal scene toward the design eye point.
 5. The head-up displaysystem of claim 1 wherein the uniaxial absorption axis is at a non-zeroangle with respect to planes defined by the first and second surface. 6.The head-up display system of claim 1 further comprising at least onereflectance modifying film disposed between the uniaxially absorbingpolarizing structure and the first surface.
 7. The head-up displaysystem of claim 1 further comprising at least one polarization modifyingfilm disposed between the uniaxially absorbing polarizing structure andthe first surface.
 8. The head-up display system of claim 1 wherein thecombiner is positioned proximate a vehicular windscreen.
 9. The head-updisplay system of claim 1 wherein the combiner is a vehicularwindscreen.
 10. The head-up display system of claim 1 wherein theuniaxially absorbing polarizing structure is a polarizing layer having ahomeotropic absorbing axis.
 11. The head-up display system of claim 1wherein the uniaxially absorbing polarizing structure comprises one ormore polarizer sections.
 12. The head-up display system of claim 1wherein the combiner is flat.
 13. The head-up display system of claim 1wherein the combiner is curved.
 14. A head-up display system,comprising: a curved combiner comprising: a transparent layer having aconcave first surface and a convex second surface and configured toallow a first image to pass therethrough in a first direction; and apolarizing layer disposed on the concave first surface, the concavefirst surface defining a tangential plane at each point of the surface,and the polarizing layer having a uniaxial absorption axis at a non-zeroangle with respect to the tangential plane, thereby configured tosuppress a refracted image created by a polarized image passing throughthe transparent layer and reflecting off the convex second surface; anda polarized image generation system configured to project the polarizedimage onto the combiner, wherein a reflected image and the first imageare combined in the first direction.
 15. An optical window having anassociated design eye point, comprising: a light transmitting elementhaving a first surface and a second surface; and a polarizing structuredisposed within the light transmitting element between the first surfaceand the second surface, the polarizing structure having a plurality ofoverlapping polarizer sections each having an absorption axis dependingon a position within the light transmitting element; wherein the lighttransmitting element and polarizing structure are configured to: passlight of arbitrary polarization through the first surface, secondsurface and design eyepoint without its polarization being substantiallychanged by the polarizing structure; and pass light through the firstsurface, second surface and polarizing structure but not the designeyepoint such that it is at least partially polarized and attenuated bythe polarizing structure.
 16. The optical window of claim 15, furthercomprising: a polarized projector; wherein a portion of the light raysexiting the projector are reflected by the optical window toward thedesign eye point prior to reaching the polarizing structure; and theportion of the light exiting the projector that reaches the polarizingstructure is substantially absorbed by the polarizing structure.
 17. Thehead-up display system of claim 14, wherein the uniaxial absorption axisof the polarizing layer varies across an area of the concave firstsurface.
 18. The head-up display system of claim 17, wherein theuniaxial absorption axis of the polarizing layer is normal relative tothe tangential plane of the concave first surface across the area.